View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 21263U 91032A 22141.89922513 .00000167 00000-0 87575-4 0 9998
2 21263 98.5136 142.4676 0014718 59.8886 300.3751 14.25989648612940
Epoch (UTC): | 21 May 2022 21:34:53 |
Eccentricity: | 0.0014718 |
inclination: | 98.5136° |
perigee height: | 794 km |
apogee height: | 816 km |
right ascension of ascending node: | 142.4676° |
argument of perigee: | 59.8886° |
revolutions per day: | 14.25989648 |
mean anomaly at epoch: | 300.3751° |
orbit number at epoch: | 61294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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